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 in relationship to the slat end (Fig. 505).
 NOTE: The seal must touch the adjacent slat or structure____
 before you make these marks.
 (e)  Move the flap control lever to the 10-unit position to fully
 extend the slats.
 (f)  Move the flap control lever to the 5-unit detent.
 (g)  Release the pressure from hydraulic system B when the leading
 edge slats are halfway between the fully extended and the
 intermediate position (AMM 27-81-00/201).
 NOTE: The retraction of the slat removes the load from the rod____
 end bolt of the slat actuator.
 (h)  Remove the fasteners that hold the electrical connector bracket
 to the slat structure.
 (i)  Disconnect the electrical connector (Ref 27-81-41 R/I).

 WARNING: MAKE SURE THAT YOU HOLD THE LEADING EDGE SLAT IN ITS
_______ POSITION. IF YOU DO NOT HOLD THE LEADING EDGE SLAT, IT WILL FALL AND CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (j)  
Hold the slat in its position.

 (k)  
Remove the rod end bolt that connects the slat to the slat actuator.

 (l)  
Manually extend the slat so the seal does not touch the adjacent slat or structure.

 (m)  
Measure the distance from the end of the slat to the marks on the spring-loaded seal (Fig. 505).

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A 737-300/400/500MAINTENANCE MANUAL
 (n)  Find the number of washers to remove or add below the seal bolt
 head to get the correct clearance between the seal and the bolt
 head.
 NOTE: The distance between the mark on the seal and the end of____
 the slat (when the seal is fully expanded, not touching
 adjacent slat) is the same as the distance between the
 seal and the bolthead washers (when the seal is
 compressed between adjacent slats).
 (o)  Manually extend the slat to get access to the end seal bolts.
 (p)  Remove the bolts that hold the seal (s) in place.
 (q)  Add or remove the washers.
 NOTE: The minimun number of washers to be installed under the____
 bolthead is one washer of 0.050 inch thickness.
 The maximum number of washers to be installed under the
 bolthead is one washer of 0.050 inch thickness
 (installed first on the bolt) plus eight washers of
 0.060 inch thickness.
 (r)  Tighten the bolts to 30-40 pound-inches.
 (s)  Compress the spring-loaded seal.
 (t)  Manually retract the slat to the same position as the remaining
 slats.
 (u)  Attach the slat actuator to the slat with the clamp up bushing,
 bolt head and retainer.
 NOTE: The clamp-up bushing, bolt head, and retainer must be____
 on the same side.
 (v)  Tighten the nut to 540-600 pound-inches.
 (w)  Put the electrical connector bracket in its position.
 (x)  Install the fasteners that hold the bracket to the slat
 actuator.
 (y)  Install the electrical connector.

 S 285-238
 (53)
 Make sure the clearances between the slat proximity sensors and the slat auxiliary track targets are correct and adjust any out of adjustment clearance if necessary (AMM 27-88-11/401).

 S 735-236

 (54)
 Do the flap and slat system tests (in primary and alternate modes) and the usual operation time test for flaps and slats given in this airplane maintenance manual.

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A
737-300/400/500MAINTENANCE MANUAL
 K.  AIRPLANES WITH SPRING LOADED SEALS AND SHIMS BELOW THE UPSTOP ADJUSTMENT BOLT HEADS (PER DWG. 65C26600, SHEET 3); Adjust the Leading Edge Slats
 S 865-229
 (1)  
Make sure you follow the safety warnings and cautions, and you complete the steps for the removal/installation of actuator locks, and the steps for applying/releasing hydraulic pressure before you cycle the slats in subsequent steps (AMM 27-81-00/201).
　
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